[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 12th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
077/06:07:32
902 -1
4 6
5 6
6
N/A -6
4 -1
0 193
6
000/00:15:01
804 0
3 0
5 187
2
Coasting Arc #1 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2011/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -937423
90 A = 6732368
70 meter
Y = 5997562
61 meter E =
0017737
Z = 2898563
63 I = 51
36240
XDOT = -5636
092403 Wp = 83
68200
YDOT = 1554
916199 meter/sec RA = 301
32196 deg
ZDOT = -5011
940658 TA = 62
83846
MA = 62
65772
Ha = 194
046 n
mi
Hp = 184
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3075537
72 X = -1018500
70
Y = 19677042
69 feet Y = 5986626
61 meter
Z = 9509723
20 Z = 2893812
38
XDOT = -18491
116809 XDOT = -5628
713964
YDOT = 5101
431100 feet/sec YDOT = 1491
930968 meter/sec
ZDOT = -16443
374863 ZDOT = -5039
302752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7149429
07 X = -2179145
98
Y = 18598332
82 feet Y = 5668771
84 meter
Z = 9490387
61 Z = 2892670
14
XDOT = -17694
499839 XDOT = -5393
283551
YDOT = 1692
411486 feet/sec YDOT = 515
847021 meter/sec
ZDOT = -16553
838337 ZDOT = -5045
609925
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11070
53769854
00016717 00000-0 10270-3 0 9003
2 25544 51
6461 301
7936 0005806 49
0101 311
1563 15
72658146 25538
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
53769854 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 301
7936 deg
Eccentricity:
0005806
Arg of perigee: 49
0101 deg
Mean anomaly: 311
1563 deg
Mean motion: 15
72658146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 295
Coasting Arc #2 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2011/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4796460
39 A = 6728453
62 meter
Y = -2274849
36 meter E =
0014532
Z = 4121014
33 I = 51
33398
XDOT = -5
184661 Wp = 86
31377
YDOT = 6748
239703 meter/sec RA = 296
22425 deg
ZDOT = 3720
796656 TA = 325
44022
MA = 325
53460
Ha = 193
911 n
mi
Hp = 184
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15736418
62 X = 4801522
77
Y = -7463416
54 feet Y = -2221183
93 meter
Z = 13520388
22 Z = 4144327
70
XDOT = -17
010044 XDOT = -98
719147
YDOT = 22139
894039 feet/sec YDOT = 6747
658923 meter/sec
ZDOT = 12207
338110 ZDOT = 3720
543953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16791425
39 X = 5118026
46
Y = -4339455
86 feet Y = -1322666
14 meter
Z = 13614533
09 Z = 4149709
69
XDOT = -4628
249867 XDOT = -1410
690560
YDOT = 20492
195600 feet/sec YDOT = 6246
021219 meter/sec
ZDOT = 12206
141128 ZDOT = 3720
431816
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11071
55439042
00016717 00000-0 10270-3 0 9010
2 25544 51
6454 296
5824 0005770 51
8916 308
2766 15
72676237 25692
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
55439042 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 296
5824 deg
Eccentricity:
0005770
Arg of perigee: 51
8916 deg
Mean anomaly: 308
2766 deg
Mean motion: 15
72676237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 326
Coasting Arc #3 (Orbit 2583)
---------------------------------------
Vector Time (GMT): 2011/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -881217
21 A = 6730176
15 meter
Y = -5647432
91 meter E =
0010123
Z = -3559223
94 I = 51
32734
XDOT = 5171
249692 Wp = 75
28535
YDOT = -3586
434112 meter/sec RA = 291
02477 deg
ZDOT = 4423
298337 TA = 242
10078
MA = 242
20333
Ha = 193
820 n
mi
Hp = 183
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2891132
59 X = -800711
22
Y = -18528323
20 feet Y = -5656837
24 meter
Z = -11677243
91 Z = -3563309
04
XDOT = 16966
042295 XDOT = 5189
482250
YDOT = -11766
516114 feet/sec YDOT = -3528
503927 meter/sec
ZDOT = 14512
133650 ZDOT = 4448
464364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 442835
86 X = 134976
37
Y = -18737110
90 feet Y = -5711071
40 meter
Z = -11693588
19 Z = -3564205
68
XDOT = 17301
063336 XDOT = 5273
364105
YDOT = -8684
749815 feet/sec YDOT = -2647
111744 meter/sec
ZDOT = 14613
789846 ZDOT = 4454
283145
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11072
50750070
00016717 00000-0 10270-3 0 9024
2 25544 51
6447 291
6968 0005534 54
3130 305
8547 15
72765492 25842
Satellite: ISS
Catalog Number: 25544
Epoch time: 11072
50750070 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 291
6968 deg
Eccentricity:
0005534
Arg of perigee: 54
3130 deg
Mean anomaly: 305
8547 deg
Mean motion: 15
72765492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2584
Checksum: 310
Coasting Arc #4 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2011/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4127717
47 A = 6729791
54 meter
Y = 3904244
58 meter E =
0010867
Z = -3619110
96 I = 51
31572
XDOT = -1902
497801 Wp = 68
74405
YDOT = -6043
091097 meter/sec RA = 285
92776 deg
ZDOT = -4355
977471 TA = 154
74744
MA = 154
69427
Ha = 193
760 n
mi
Hp = 183
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13542380
16 X = -4153488
02
Y = 12809201
39 feet Y = 3857941
68 meter
Z = -11873723
62 Z = -3639225
84
XDOT = -6241
790685 XDOT = -1813
621226
YDOT = -19826
414361 feet/sec YDOT = -6063
869253 meter/sec
ZDOT = -14291
264668 ZDOT = -4365
003476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15313759
94 X = -4667634
03
Y = 10536779
84 feet Y = 3211610
50 meter
Z = -11955000
64 Z = -3643884
20
XDOT = -2201
186302 XDOT = -670
921585
YDOT = -19430
567016 feet/sec YDOT = -5922
436826 meter/sec
ZDOT = -14327
549477 ZDOT = -4367
037081
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11073
52411434
00016717 00000-0 10270-3 0 9036
2 25544 51
6437 286
4858 0005473 57
6328 302
5363 15
72815986 26001
Satellite: ISS
Catalog Number: 25544
Epoch time: 11073
52411434 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 286
4858 deg
Eccentricity:
0005473
Arg of perigee: 57
6328 deg
Mean anomaly: 302
5363 deg
Mean motion: 15
72815986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 311
Coasting Arc #5 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2011/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2379407
28 A = 6728114
46 meter
Y = 4819153
79 meter E =
0015912
Z = 4038132
74 I = 51
30396
XDOT = -4120
899711 Wp = 71
07635
YDOT = 5260
545119 meter/sec RA = 280
72541 deg
ZDOT = -3832
415296 TA = 58
60171
MA = 58
44618
Ha = 193
547 n
mi
Hp = 183
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7806454
32 X = 2305725
62
Y = 15810872
00 feet Y = 4845350
03 meter
Z = 13248466
99 Z = 4049512
40
XDOT = -13520
012174 XDOT = -4160
801049
YDOT = 17259
006295 feet/sec YDOT = 5214
239386 meter/sec
ZDOT = -12573
540996 ZDOT = -3852
531457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5439619
33 X = 1657995
97
Y = 16736745
69 feet Y = 5101360
09 meter
Z = 13294290
70 Z = 4052099
80
XDOT = -14505
871389 XDOT = -4421
389599
YDOT = 14811
727295 feet/sec YDOT = 4514
614480 meter/sec
ZDOT = -12654
850058 ZDOT = -3857
198298
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11074
54068613
00016717 00000-0 10270-3 0 9047
2 25544 51
6440 281
2738 0005387 59
6210 300
5485 15
72919566 26160
Satellite: ISS
Catalog Number: 25544
Epoch time: 11074
54068613 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 281
2738 deg
Eccentricity:
0005387
Arg of perigee: 59
6210 deg
Mean anomaly: 300
5485 deg
Mean motion: 15
72919566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 311
Coasting Arc #6 (Orbit 2631)
---------------------------------------
Vector Time (GMT): 2011/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2979303
90 A = 6730990
11 meter
Y = -5186659
42 meter E =
0018155
Z = 3067294
03 I = 51
30792
XDOT = 3443
591564 Wp = 78
83851
YDOT = 4873
487717 meter/sec RA = 275
62402 deg
ZDOT = 4875
141442 TA = 316
93741
MA = 317
07932
Ha = 193
467 n
mi
Hp = 183
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9774619
10 X = 3022180
65
Y = -17016599
16 feet Y = -5153103
05 meter
Z = 10063300
63 Z = 3081871
75
XDOT = 11297
872585 XDOT = 3365
157320
YDOT = 15989
132931 feet/sec YDOT = 4911
557902 meter/sec
ZDOT = 15994
558536 ZDOT = 4891
679124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11730567
29 X = 3575476
91
Y = -15694322
92 feet Y = -4783629
63 meter
Z = 10122246
00 Z = 3085260
58
XDOT = 8008
977152 XDOT = 2441
136236
YDOT = 16389
085080 feet/sec YDOT = 4995
393132 meter/sec
ZDOT = 16061
211561 ZDOT = 4895
457284
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11075
55721864
00016717 00000-0 10270-3 0 9054
2 25544 51
6423 276
0615 0005296 64
0955 296
0753 15
72964759 26321
Satellite: ISS
Catalog Number: 25544
Epoch time: 11075
55721864 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 276
0615 deg
Eccentricity:
0005296
Arg of perigee: 64
0955 deg
Mean anomaly: 296
0753 deg
Mean motion: 15
72964759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 329
Coasting Arc #7 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2011/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3530023
53 A = 6726371
85 meter
Y = -3633412
76 meter E =
0014058
Z = -4437894
19 I = 51
28982
XDOT = 2625
695669 Wp = 95
58690
YDOT = -6470
716987 meter/sec RA = 270
42248 deg
ZDOT = 3216
588325 TA = 206
79894
MA = 206
87163
Ha = 193
492 n
mi
Hp = 183
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11581442
04 X = -3467573
62
Y = -11920645
53 feet Y = -3672538
93 meter
Z = -14560020
31 Z = -4454890
60
XDOT = 8614
487104 XDOT = 2682
232024
YDOT = -21229
386441 feet/sec YDOT = -6441
038403 meter/sec
ZDOT = 10553
111302 ZDOT = 3229
481721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10169353
78 X = -3099619
03
Y = -13069632
48 feet Y = -3983623
98 meter
Z = -14628558
77 Z = -4458784
71
XDOT = 9794
690924 XDOT = 2985
421794
YDOT = -19464
344015 feet/sec YDOT = -5932
732056 meter/sec
ZDOT = 10605
272556 ZDOT = 3232
487075
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11076
51018035
00016717 00000-0 10270-3 0 9061
2 25544 51
6411 271
1739 0005388 68
0952 292
0783 15
73012371 26474
Satellite: ISS
Catalog Number: 25544
Epoch time: 11076
51018035 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 271
1739 deg
Eccentricity:
0005388
Arg of perigee: 68
0952 deg
Mean anomaly: 292
0783 deg
Mean motion: 15
73012371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 299
Coasting Arc #8 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2011/077/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4057215
41 A = 6728223
69 meter
Y = -2255873
47 meter E =
0011942
Z = -4881087
12 I = 51
28667
XDOT = 1346
722747 Wp = 100
19244
YDOT = -7234
190165 meter/sec RA = 266
50969 deg
ZDOT = 2226
533468 TA = 191
58120
MA = 191
60870
Ha = 193
584 n
mi
Hp = 187
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13311074
19 X = -4007977
25
Y = -7401159
66 feet Y = -2300969
02 meter
Z = -16014065
35 Z = -4900676
84
XDOT = 4418
381715 XDOT = 1416
700839
YDOT = -23734
219702 feet/sec YDOT = -7218
738745 meter/sec
ZDOT = 7304
899830 ZDOT = 2233
246617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7757358
90 X = 2364442
99
Y = -13009521
68 feet Y = -3965302
21 meter
Z = -16093100
33 Z = -4905176
98
XDOT = 22657
933194 XDOT = 6906
138037
YDOT = 4450
816087 feet/sec YDOT = 1356
608743 meter/sec
ZDOT = 7332
119323 ZDOT = 2234
829970
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11077
27252726
00016717 00000-0 10270-3 0 9073
2 25544 51
6436 267
2645 0001398 353
1079 7
0063 15
71732482 26596
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
27252726 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 267
2645 deg
Eccentricity:
0001398
Arg of perigee: 353
1079 deg
Mean anomaly: 7
0063 deg
Mean motion: 15
71732482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 313
Coasting Arc #9 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2011/078/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -36722
24 A = 6737801
77 meter
Y = 6611861
42 meter E =
0007843
Z = -1280896
42 I = 51
32265
XDOT = -4891
830038 Wp = 137
48503
YDOT = -1150
910103 meter/sec RA = 261
39698 deg
ZDOT = -5827
126029 TA = 56
61523
MA = 56
54020
Ha = 193
533 n
mi
Hp = 187
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -120479
78 X = -104432
31
Y = 21692458
72 feet Y = 6611072
00 meter
Z = -4202416
08 Z = -1281240
19
XDOT = -16049
311147 XDOT = -4850
289983
YDOT = -3775
951780 feet/sec YDOT = -1205
382055 meter/sec
ZDOT = -19117
867550 ZDOT = -5850
789189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21690283
94 X = -6611198
54
Y = -310384
98 feet Y = -94605
34 meter
Z = -4203905
96 Z = -1281350
54
XDOT = 3911
848327 XDOT = 1192
331370
YDOT = -14314
781473 feet/sec YDOT = -4363
145393 meter/sec
ZDOT = -19213
365371 ZDOT = -5856
233765
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11078
28980658
00016717 00000-0 10270-3 0 9088
2 25544 51
6439 262
0574 0001387 353
2426 6
8717 15
71774588 26752
Satellite: ISS
Catalog Number: 25544
Epoch time: 11078
28980658 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 262
0574 deg
Eccentricity:
0001387
Arg of perigee: 353
2426 deg
Mean anomaly: 6
8717 deg
Mean motion: 15
71774588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 344
Coasting Arc #10 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2011/079/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4238826
90 A = 6726255
74 meter
Y = -259413
60 meter E =
0003800
Z = 5214249
64 I = 51
29048
XDOT = 1295
683045 Wp = 40
33004
YDOT = 7559
918883 meter/sec RA = 256
23599 deg
ZDOT = -674
056410 TA = 56
12948
MA = 56
09333
Ha = 193
219 n
mi
Hp = 187
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13906912
39 X = 4216082
93
Y = -851094
50 feet Y = -212138
94 meter
Z = 17107118
25 Z = 5234786
53
XDOT = 4250
928626 XDOT = 1214
324721
YDOT = 24802
883476 feet/sec YDOT = 7573
953008 meter/sec
ZDOT = -2211
471162 ZDOT = -667
960649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 951014
20 X = 289869
13
Y = 13797785
52 feet Y = 4205565
03 meter
Z = 17190019
08 Z = 5239517
82
XDOT = -23764
910234 XDOT = -7243
544639
YDOT = 4375
391646 feet/sec YDOT = 1333
619374 meter/sec
ZDOT = -2186
975635 ZDOT = -666
590173
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11079
30704457
00016717 00000-0 10270-3 0 9094
2 25544 51
6437 256
8502 0001583 352
4136 7
7002 15
71891808 26919
Satellite: ISS
Catalog Number: 25544
Epoch time: 11079
30704457 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 256
8502 deg
Eccentricity:
0001583
Arg of perigee: 352
4136 deg
Mean anomaly: 7
7002 deg
Mean motion: 15
71891808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 307
Coasting Arc #11 (Orbit 2705)
---------------------------------------
Vector Time (GMT): 2011/080/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2252356
88 A = 6738118
34 meter
Y = -6342559
28 meter E =
0013255
Z = -95217
43 I = 51
33969
XDOT = 4506
536231 Wp = 39
12351
YDOT = -1683
614687 meter/sec RA = 251
09761 deg
ZDOT = 6011
048539 TA = 319
83851
MA = 319
93640
Ha = 193
365 n
mi
Hp = 186
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7389622
31 X = -2180803
23
Y = -20808921
52 feet Y = -6367346
43 meter
Z = -312393
15 Z = -105984
84
XDOT = 14785
223854 XDOT = 4495
827234
YDOT = -5523
670233 feet/sec YDOT = -1633
279056 meter/sec
ZDOT = 19721
287858 ZDOT = 6032
915444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20621784
99 X = 6285520
06
Y = -7894981
68 feet Y = -2406390
42 meter
Z = -355767
09 Z = -108437
81
XDOT = 5304
695948 XDOT = 1616
871325
YDOT = 13023
601848 feet/sec YDOT = 3969
593843 meter/sec
ZDOT = 19809
578919 ZDOT = 6037
959655
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11080
26067142
00016717 00000-0 10270-3 0 9106
2 25544 51
6444 251
9680 0001708 357
4206 2
6947 15
71912333 27068
Satellite: ISS
Catalog Number: 25544
Epoch time: 11080
26067142 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 251
9680 deg
Eccentricity:
0001708
Arg of perigee: 357
4206 deg
Mean anomaly: 2
6947 deg
Mean motion: 15
71912333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2706
Checksum: 288
Coasting Arc #12 (Orbit 2721)
---------------------------------------
Vector Time (GMT): 2011/081/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3420885
09 A = 6726061
21 meter
Y = 2564182
50 meter E =
0014957
Z = -5205501
57 I = 51
31144
XDOT = -3717
077563 Wp = 76
51775
YDOT = -6675
100381 meter/sec RA = 245
96345 deg
ZDOT = -843
952707 TA = 185
38812
MA = 185
40423
Ha = 193
293 n
mi
Hp = 186
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11223376
28 X = -3424016
61
Y = 8412672
24 feet Y = 2525910
13 meter
Z = -17078417
22 Z = -5222128
07
XDOT = -12195
136363 XDOT = -3638
059285
YDOT = -21899
935633 feet/sec YDOT = -6716
225254 meter/sec
ZDOT = -2768
873709 ZDOT = -861
817763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8868218
73 X = -2703033
07
Y = -10760747
62 feet Y = -3279875
87 meter
Z = -17145570
03 Z = -5225969
74
XDOT = 20588
725870 XDOT = 6275
443645
YDOT = -12433
906315 feet/sec YDOT = -3789
854645 meter/sec
ZDOT = -2840
897129 ZDOT = -865
905445
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11081
27783237
00016717 00000-0 10270-3 0 9119
2 25544 51
6449 246
7604 0001823 359
6664
4497 15
71999058 27224
Satellite: ISS
Catalog Number: 25544
Epoch time: 11081
27783237 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 246
7604 deg
Eccentricity:
0001823
Arg of perigee: 359
6664 deg
Mean anomaly:
4497 deg
Mean motion: 15
71999058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2722
Checksum: 327
Coasting Arc #13 (Orbit 2737)
---------------------------------------
Vector Time (GMT): 2011/082/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4116837
36 A = 6737030
68 meter
Y = 5151425
74 meter E =
0013308
Z = 1351881
13 I = 51
36205
XDOT = -3084
416860 Wp = 113
11365
YDOT = 4000
041773 meter/sec RA = 240
80136 deg
ZDOT = -5809
376169 TA = 51
98781
MA = 51
86773
Ha = 193
302 n
mi
Hp = 186
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13506684
26 X = 4052359
97
Y = 16901003
07 feet Y = 5197102
28 meter
Z = 4435305
56 Z = 1371723
79
XDOT = -10119
477887 XDOT = -3100
695950
YDOT = 13123
496629 feet/sec YDOT = 3965
458578 meter/sec
ZDOT = -19059
633102 ZDOT = -5824
400047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16078437
16 X = -4900707
65
Y = 14451364
31 feet Y = 4404775
84 meter
Z = 4515339
22 Z = 1376275
39
XDOT = -12635
095892 XDOT = -3851
177228
YDOT = -8043
074891 feet/sec YDOT = -2451
529227 meter/sec
ZDOT = -19120
340302 ZDOT = -5827
879724
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11082
29495375
00016717 00000-0 10270-3 0 9126
2 25544 51
6449 241
5528 0001761 3
8337 356
2838 15
72008591 27380
Satellite: ISS
Catalog Number: 25544
Epoch time: 11082
29495375 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 241
5528 deg
Eccentricity:
0001761
Arg of perigee: 3
8337 deg
Mean anomaly: 356
2838 deg
Mean motion: 15
72008591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2738
Checksum: 320
Coasting Arc #14 (Orbit 2753)
---------------------------------------
Vector Time (GMT): 2011/083/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1819967
09 A = 6727205
97 meter
Y = -4254965
91 meter E =
0005899
Z = 4878052
93 I = 51
34587
XDOT = 5502
476196 Wp = 104
83591
YDOT = 4907
594703 meter/sec RA = 235
69093 deg
ZDOT = 2224
071158 TA = 323
44006
MA = 323
48031
Ha = 193
154 n
mi
Hp = 186
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5971020
63 X = 1843715
04
Y = -13959861
91 feet Y = -4234480
95 meter
Z = 16004110
67 Z = 4886952
17
XDOT = 18052
743425 XDOT = 5436
385478
YDOT = 16101
032490 feet/sec YDOT = 4968
757287 meter/sec
ZDOT = 7296
821385 ZDOT = 2250
641358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14365476
33 X = 4378597
19
Y = 4796949
29 feet Y = 1462110
14 meter
Z = 16040098
42 Z = 4889022
00
XDOT = -14335
835933 XDOT = -4369
562792
YDOT = 18133
195457 feet/sec YDOT = 5526
997975 meter/sec
ZDOT = 7404
028318 ZDOT = 2256
747831
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11083
31203104
00016717 00000-0 10270-3 0 9138
2 25544 51
6451 236
3447 0002031 4
7745 355
3436 15
72098049 27548
Satellite: ISS
Catalog Number: 25544
Epoch time: 11083
31203104 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 236
3447 deg
Eccentricity:
0002031
Arg of perigee: 4
7745 deg
Mean anomaly: 355
3436 deg
Mean motion: 15
72098049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2754
Checksum: 280
Coasting Arc #15 (Orbit 2768)
---------------------------------------
Vector Time (GMT): 2011/084/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5306273
93 A = 6734638
48 meter
Y = -3312194
14 meter E =
0006928
Z = -2490275
55 I = 51
38942
XDOT = 951
831118 Wp = 36
62685
YDOT = -5498
953787 meter/sec RA = 230
51040 deg
ZDOT = 5298
777045 TA = 295
12102
MA = 295
19288
Ha = 193
063 n
mi
Hp = 186
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17409035
19 X = -5256744
74
Y = -10866778
69 feet Y = -3371255
27 meter
Z = -8170195
36 Z = -2515932
82
XDOT = 3122
805505 XDOT = 987
510403
YDOT = -18041
186964 feet/sec YDOT = -5488
110159 meter/sec
ZDOT = 17384
439125 ZDOT = 5303
487860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9202531
40 X = 2804931
57
Y = -18296774
15 feet Y = -5576856
76 meter
Z = -8273750
60 Z = -2521839
18
XDOT = 16909
043918 XDOT = 5153
876586
YDOT = 653
843501 feet/sec YDOT = 199
291499 meter/sec
ZDOT = 17403
532756 ZDOT = 5304
596784
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11084
26550239
00016717 00000-0 10270-3 0 9148
2 25544 51
6446 231
4618 0002213 2
0474 358
0697 15
72165339 27692
Satellite: ISS
Catalog Number: 25544
Epoch time: 11084
26550239 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 231
4618 deg
Eccentricity:
0002213
Arg of perigee: 2
0474 deg
Mean anomaly: 358
0697 deg
Mean motion: 15
72165339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2769
Checksum: 304
Coasting Arc #16 (Orbit 2784)
---------------------------------------
Vector Time (GMT): 2011/085/06:15:03
804
Vector Time (MET): N/A
Weight (LBS) : 919647
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 197764
33 A = 6729048
89 meter
Y = 5143433
30 meter E =
0010039
Z = -4344764
96 I = 51
39049
XDOT = -6383
942335 Wp = 57
68823
YDOT = -2619
096990 meter/sec RA = 225
41663 deg
ZDOT = -3391
560115 TA = 177
94659
MA = 177
94246
Ha = 193
036 n
mi
Hp = 186
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 648833
09 X = 161340
63
Y = 16874781
18 feet Y = 5145441
01 meter
Z = -14254478
21 Z = -4343892
89
XDOT = -20944
692701 XDOT = -6337
705219
YDOT = -8592
837895 feet/sec YDOT = -2690
227701 meter/sec
ZDOT = -11127
165732 ZDOT = -3422
460558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16690337
02 X = -5087214
72
Y = 2590452
55 feet Y = 789569
94 meter
Z = -14251020
28 Z = -4343710
98
XDOT = 6427
444096 XDOT = 1959
084961
YDOT = -20480
980369 feet/sec YDOT = -6242
602816 meter/sec
ZDOT = -11251
916383 ZDOT = -3429
584114
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11085
28249743
00016717 00000-0 10270-3 0 9157
2 25544 51
6437 226
2531 0002257 2
6605 357
4569 15
72229408 27855
Satellite: ISS
Catalog Number: 25544
Epoch time: 11085
28249743 = yrday
fracday
Element set: 915
Inclination: 51
6437 deg
RA of node: 226
2531 deg
Eccentricity:
0002257
Arg of perigee: 2
6605 deg
Mean anomaly: 357
4569 deg
Mean motion: 15
72229408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2785
Checksum: 316
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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